A supercapacitor electrode mechanism comprising an electrically conductive, porous substrate, having one or more metallic oxides deposited on a first surface and a chemically reduced graphene oxide deposited on a second surface, to thereby provide an electrical double layer associated with the substrate. The substrate may be carbon paper or a similar substance. The layers of the supercapacitor are optionally rolled into an approximately cylindrical structure.
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1. A method for fabricating a supercapacitor, the method comprising:
providing an electrically conductive substrate, having spaced apart first and second surfaces;
providing a layer of metal oxides, including at least one of MnO2 and Co3O4, contiguous to the first substrate surface; and
providing a layer of chemically reduced graphene oxide (rGO) contiguous to the second substrate surface, to thereby provide an electrical double layer associated with the substrate.
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The invention described herein was made in the performance of work under a NASA contract and by an employee of the United States Government and is subject to the provisions of Public Law 96-517 (35 U.S.C. §202) and may be manufactured and used by or for the Government for governmental purposes without the payment of any royalties thereon or therefore. In accordance with 35 U.S.C. §202, the contractor elected not to retain title.
This invention relates to nanofabrication of an electrode suitable for use in a supercapacitor.
A supercapacitor requires use of a substance that has a relatively high power density, which can be achieved with some materials, and simultaneously a relatively high energy density. Achievement of both of these conditions with a single material has not been possible in the prior art.
The invention meets these needs by providing a procedure for nanofabrication of an electrode mechanism, for use in a supercapacitor (SC) that has relatively high power density (100-200 KW/Kgm or higher) and simultaneously has relatively energy density (20 KW-hr/KGM or higher). The procedure includes the steps of: (1) providing a porous, electrically conductive substrate that has first and second, spaced apart surfaces; (2) depositing one or more selected metal oxides, including at least one of MnO2 and Co3O4, on the first substrate surface; and (3) depositing an assembly of chemically reduced graphene oxide (rGO) on the second substrate surface, to thereby provide an electrical double layer associated with the substrate.
In step 12, one or more selected metal oxides, including at least one of MnO2 and Co3O4, is deposited on the first substrate surface. The metal oxide has an associated specific capacity of around 300 Farads/gm.
In a third step 13, an assembly of flakes or chips of reduced graphene oxide (rGO) is deposited on the second substrate surface, with individual flake thicknesses in a range 1-15 μm, depending upon the electrolyte. Deposition of the rGO can, for example, be achieved by deposit of graphene oxide (GO) on the substrate second surface, followed by electrophoretic deposition (EPD), such as cathodic deposition using an electrolyte such as a room temperature ionic liquid (RTIL).
An RTIL is a room temperature, liquid, solvent-free electrolyte. Examples of RTILs are 1-butyl-1-methylpyrrolldinium bis(trifluoromethylsulfonyl)imide, Methyltrioctylammonium bis(trifluoromethylsulfonyl)imide, ammonium ions, and methyl imidazole.
The reducing agent may be hydrazine, sodium borohydride, or a similar substance. The rGO helps provide an electrical double layer associated with the substrate.
This fabrication procedure also provides a three-layer (more generally, a multi-layer) cylindrical embodiment 30 in
In an embodiment, illustrated in
Ideally, the system should operate at temperatures in a range −40° C.<T<100° C., should operate at voltages in a range −3 to +7 Volts, and should rely upon non-toxic materials for fabrication. The system should be mechanically flexible and have a relatively small form factor.
It will be appreciated to those skilled in the art that the preceding examples and embodiment are exemplary and not limiting to the scope of the present invention. It is intended that all permutations, enhancements, equivalents, combinations, and improvements thereto that are apparent to those skilled in the art upon a reading of the specification and a study of the drawings are included within the true spirit and scope of the present invention.
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Mar 01 2013 | The United States of America as Represented by the Administrator of the National Aeronautics & Space Administration (NASA) | (assignment on the face of the patent) | / | |||
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